DE8001995U1 - Bearing body for a plain bearing with high thermal conductivity - Google Patents
Bearing body for a plain bearing with high thermal conductivityInfo
- Publication number
- DE8001995U1 DE8001995U1 DE8001995U DE8001995DU DE8001995U1 DE 8001995 U1 DE8001995 U1 DE 8001995U1 DE 8001995 U DE8001995 U DE 8001995U DE 8001995D U DE8001995D U DE 8001995DU DE 8001995 U1 DE8001995 U1 DE 8001995U1
- Authority
- DE
- Germany
- Prior art keywords
- bearing
- copper
- bearing body
- white metal
- iron
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 20
- 229910001361 White metal Inorganic materials 0.000 claims description 18
- 239000010969 white metal Substances 0.000 claims description 18
- 229910052802 copper Inorganic materials 0.000 claims description 11
- 239000010949 copper Substances 0.000 claims description 11
- RYGMFSIKBFXOCR-UHFFFAOYSA-N copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 10
- 229910052742 iron Inorganic materials 0.000 claims description 10
- 229910000881 Cu alloy Inorganic materials 0.000 claims description 6
- 229910052804 chromium Inorganic materials 0.000 claims description 2
- 239000011651 chromium Substances 0.000 claims description 2
- VYZAMTAEIAYCRO-UHFFFAOYSA-N chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 2
- 229910052718 tin Inorganic materials 0.000 claims description 2
- ATJFFYVFTNAWJD-UHFFFAOYSA-N tin hydride Chemical group [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 claims description 2
- QCWXUUIWCKQGHC-UHFFFAOYSA-N zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims description 2
- 229910052726 zirconium Inorganic materials 0.000 claims description 2
- WATWJIUSRGPENY-UHFFFAOYSA-N antimony Chemical compound [Sb] WATWJIUSRGPENY-UHFFFAOYSA-N 0.000 claims 1
- 229910052787 antimony Inorganic materials 0.000 claims 1
- 229910001018 Cast iron Inorganic materials 0.000 description 4
- 229910000640 Fe alloy Inorganic materials 0.000 description 3
- 229910000831 Steel Inorganic materials 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 239000010959 steel Substances 0.000 description 3
- 229910000906 Bronze Inorganic materials 0.000 description 2
- 241000282898 Sus scrofa Species 0.000 description 2
- 239000010974 bronze Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- 229910000897 Babbitt (metal) Inorganic materials 0.000 description 1
- 229910000978 Pb alloy Inorganic materials 0.000 description 1
- 229910001245 Sb alloy Inorganic materials 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000000969 carrier Substances 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 238000011156 evaluation Methods 0.000 description 1
- 238000005755 formation reaction Methods 0.000 description 1
- 230000017525 heat dissipation Effects 0.000 description 1
- 238000001802 infusion Methods 0.000 description 1
- 229910000765 intermetallic Inorganic materials 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 230000002028 premature Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/02—Parts of sliding-contact bearings
- F16C33/04—Brasses; Bushes; Linings
- F16C33/06—Sliding surface mainly made of metal
- F16C33/12—Structural composition; Use of special materials or surface treatments, e.g. for rust-proofing
- F16C33/121—Use of special materials
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/01—Layered products comprising a layer of metal all layers being exclusively metallic
- B32B15/013—Layered products comprising a layer of metal all layers being exclusively metallic one layer being formed of an iron alloy or steel, another layer being formed of a metal other than iron or aluminium
- B32B15/015—Layered products comprising a layer of metal all layers being exclusively metallic one layer being formed of an iron alloy or steel, another layer being formed of a metal other than iron or aluminium the said other metal being copper or nickel or an alloy thereof
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C9/00—Alloys based on copper
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C9/00—Alloys based on copper
- C22C9/06—Alloys based on copper with nickel or cobalt as the next major constituent
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/02—Parts of sliding-contact bearings
- F16C33/04—Brasses; Bushes; Linings
- F16C33/06—Sliding surface mainly made of metal
- F16C33/12—Structural composition; Use of special materials or surface treatments, e.g. for rust-proofing
- F16C33/122—Multilayer structures of sleeves, washers or liners
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/02—Parts of sliding-contact bearings
- F16C33/04—Brasses; Bushes; Linings
- F16C33/06—Sliding surface mainly made of metal
- F16C33/12—Structural composition; Use of special materials or surface treatments, e.g. for rust-proofing
- F16C33/122—Multilayer structures of sleeves, washers or liners
- F16C33/125—Details of bearing layers, i.e. the lining
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/02—Parts of sliding-contact bearings
- F16C33/04—Brasses; Bushes; Linings
- F16C33/06—Sliding surface mainly made of metal
- F16C33/14—Special methods of manufacture; Running-in
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2204/00—Metallic materials; Alloys
- F16C2204/10—Alloys based on copper
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2204/00—Metallic materials; Alloys
- F16C2204/10—Alloys based on copper
- F16C2204/12—Alloys based on copper with tin as the next major constituent
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2223/00—Surface treatments; Hardening; Coating
- F16C2223/30—Coating surfaces
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Sliding-Contact Bearings (AREA)
Description
Die Neuerung geht aus von einem Lagerkörper nach der Gattung des Anspruchs 1.The innovation is based on a bearing body according to the preamble of claim 1.
Lagerkörper (meist Lagerschalen) für Gleitlager vmrden bisher meistens entweder aus einer Kupferlegierung (z.B. Bronze) oder aus Stahl oder Gusseisen gefertigt, auf Vielehe dann eine Schicht Zinn-Weissmetall (meist Sn/Pb/Sb-Legierung) in der Regel durch Ausgiessen aufgebracht wurde. Derartige Verfahren sowie die danach hergestellten Erzeugnisse sind aus der Literatur hinlänglich bekannt (z.B. Czochralski, Lagermetalle und ihre technologische Bewertung, Springer Berlin, 1920; W.Hilgers, Abhängigkeit der Lagerwerkstoffeigenschaften in Verbundlagern von der Stützkörperknnstruktion, VDI-Berichte Nr. 248, 1975, S.149-158; H.Loewie, Aus der Praxis der Gleitlagerfertigung, Goldschmidt informiert 2/70, Nr.ll, S.25-26; W.Hilgers, Verbesserung der Bindungsfestigkeit von Stützkörpern aus Gusseisen mit LagerWerksfcoffen, Goldschmidt informiert 3/74, Nr.30, S.4-5)t Bearing bodies (mostly bearing shells) for plain bearings have so far mostly been made either from a copper alloy (e.g. bronze) or from steel or cast iron, and a layer of tin-white metal (mostly Sn / Pb / Sb alloy) has usually been poured onto polygons . Such processes as well as the products manufactured according to them are well known from the literature (e.g. Czochralski, Lagermetalle und their technological evaluation, Springer Berlin, 1920; W. Hilgers, Dependence of the bearing material properties in composite bearings on the support structure, VDI reports No. 248, 1975, S.149-158; H.Loewie, From the practice of slide bearing production, Goldschmidt informs 2/70, Nr.ll, p.25-26; W.Hilgers, Improvement of the bond strength of support bodies made of cast iron with bearing factories, Goldschmidt informs 3 / 74, No. 30, pp. 4-5) t
I Il I 4 tilt It Il fl i I* < 4 I ir III*I Il I 4 tilt It Il fl i I * < 4 I ir III *
1111/79 ßE/βΜΛ1111/79 ßE / βΜΛ
I ti· »4 i 4 4 i i * 4I ti · »4 i 4 4 ii * 4
4 14 4 «(4 4 4 « ■ 4 J Ii ti» it ti4 14 4 «(4 4 4« ■ 4 J Ii ti » it ti
Bei niedrigen Belastungen und vergleichsweise niedrigen j Temperaturen haben sich derartige herkömmliche Lagerkörper im allgemeinen gut bewahrt t Die Haftung zwischen Bronze und Zinn-Weissmetali ist ausgezeichnet, diejenige zwischen Eisenlegierungen und Zinn-Weissmetall in der Regel gut* Bei höchsten Belastungen und demzufolge höheren Temperaturen (120 ° C und mehr) hat jedoch die Kombination Kupferiegierung/Zinn-Weissmetall die unangenehme Eigenschaft, dass die in der Uebergangszone für die Haftung und Bindung verantwortliche Schicht spröder und harter intermetallischer Verbindungen in der Dicke zufolge erhöhter Diffusion zunimmt und daher der Verband durch Rissbildung und Abblättern gefährdet ist. Andererseits sind Lagerschalen aus Eisenlegierungen (Stahl, Gusseisen) Vergleichsweise schlechte Wärmeleiter, so dass der Belastung von der Temperaturseite des Zinn-Weissmetalles her bald Grenzen gesetzt sind (hoher Temperaturgradient Weissmetalloberfläche/ Stützkörperoberfläche).At low loads and comparatively low j temperatures, conventional bearing bodies of this type have generally proved their worth t The adhesion between bronze and tin-white metal is excellent, that between iron alloys and tin-white metal is generally good * At the highest loads and consequently higher temperatures (120 ° C and more), however, the combination of copper alloy / tin-white metal has the unpleasant property that the layer of brittle and hard intermetallic compounds responsible for adhesion and bonding in the transition zone increases in thickness due to increased diffusion and therefore the bond through cracking and peeling endangered is. On the other hand, bearing shells made of iron alloys (steel, cast iron) are comparatively poor heat conductors, so that the load on the temperature side of the tin-white metal will soon be limited (high temperature gradient white metal surface / support body surface).
Der Erfindung liegt die Aufgabe zugrunde, ein einfaches Verfahren zur Herstellung eines Lagerkörpers auf der Basis von Weissmetall anzugeben, welches bei hoher Wärmeleitfähigkeit und demzufolge hoher Belastbarkeit die für Zinn- f weissmetall höchstzulässigen Betriebstemperaturen auszunutzen gestattet und dank guter Bindung zwischen Lager- i werkstoff und Stützkörpermäterial eine lange Lebensdauer j und hohe Betriebssicherheit gewährleistet. jThe invention has for its object to provide a simple process for producing a bearing body on the basis of white metal, which is the f for tin white metal maximum operating temperatures allows for high thermal conductivity and consequently high load capacity to exploit and thanks to a good bond between bearing i material and Stützkörpermäterial a long service life and high operational reliability guaranteed. j
Diese Aufgabe wird durch die Merkmale des jThis task is made possible by the characteristics of the j
Anspruchs 1 gelöst. ;Claim 1 solved. ;
'§ # # t* ItIt'§ # # t * ItIt
4144 * i * 4 * 4*6 t 4144 * i * 4 * 4 * 6 t
.· ί : s ί ι ί ίί ί. · Ί: s ί ι ί ίί ί
Die Erfindung wird anhand der nachfolgenden * durch Figuren erläuterten Ausführungsbeispiele beschrieben *The invention is illustrated by the following * figures illustrated embodiments described *
Dabei zeigt:It shows:
Fig. 1 eine perspektivische Darstellung eines Lagerkörpers für eine Radiallager^Halbschäle,Fig. 1 is a perspective view of a bearing body for a radial bearing ^ half-shells,
Fig. 2 eine perspektivische Darstellung eines Lagerkörpers für ein Axiallager-Kreissegment,2 shows a perspective illustration of a bearing body for a circular axial bearing segment,
Fig. 3 einen schematischen Schnitt durch die Schichtfolge eines Lagerkörpers.3 shows a schematic section through the layer sequence of a bearing body.
In Fig. 1 ist ein Lagerkörper für eine Radiallager-Halbschale perspektivisch dargestellt. Der eine Radiallager-Halbschale 1 bildende Lagerkörper setzt sich aus einem Kupfermantel 2 als Grundkörper (Stützkörper), einer zylindrischen Eisen-Zwischenschicht 3 und einem ebenfalls zylindrischen Weissmetall-Ausguss 4 als Deckschicht zusammen, welcher die eigentliche, der Welle zugekehrte Lauffläche bildet. Die Eisen-Zwischenschicht 3 weist je nach Lagergrösse in der Regel eine Dicke von 15 bis 150 μ auf, während der Weissmetall-Ausguss 4 im allgemeinen mehrere mm dick gewählt wird. Die Zwischenschicht 3 kann auch aus einer Folge einer Lage Nickel und einer Lage Eisen bestehen, wobei das letztere auf der Seite des Weissmetall-Ausgusses 4 liegt. Weiterhin kann das Reinkupfer des Mantels 2 durch eine Kupferlegierung mit Chrom- und/oder Zirkongehalt ersetzt sein.In Fig. 1, a bearing body for a radial bearing half-shell is shown in perspective. The bearing body forming a radial bearing half-shell 1 is composed of a copper jacket 2 as the base body (support body), a cylindrical iron intermediate layer 3 and a likewise cylindrical white metal spout 4 as a cover layer, which forms the actual running surface facing the shaft. The iron intermediate layer 3 has a thickness of 15 to 150 μ , depending on the size of the bearing, while the white metal spout 4 is generally selected to be several mm thick. The intermediate layer 3 can also consist of a sequence of a layer of nickel and a layer of iron, the latter lying on the side of the white metal spout 4. Furthermore, the pure copper of the jacket 2 can be replaced by a copper alloy with a chromium and / or zirconium content.
141/79 ßfi/öif141/79 ßfi / öif
I · 1 «ilI · 1 «il
I Ol 11 t lit I Ol 11 t lit i Ii I
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itit i Ii I
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itit
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i · I ι t I ))I I) i I ι t I )) II)
Pig. 2 zeigt die perspektivische Darstellung eines Lagerkörpers für ein Segmentlager* Das Axiallager-Kreissegmerit besteht aus einem Kupferblock 6 als Grundkörper (Stützkörper1) > einer ebenen Eisen-Zwischenschicht 7 und einem ebenen Aufguss als Weissmetall-Deckschicht 8. Bezüglich Dicke der einzelnen Schichten und Variation der Werkstoff Zusammensetzung wird auf den Text unter Pig. I verwiesen* Pig. 2 shows the perspective view of a bearing body for a segment bearing * The axial bearing circular segment consists of a copper block 6 as a base body (support body 1 )> a flat iron intermediate layer 7 and a flat infusion as a white metal cover layer 8. With regard to the thickness of the individual layers and variations the material composition is shown on the text under Pig. I referred *
In Fig. 3 ist ein Schnitt durch die Schichtfolge eines IQ Lagerkörpers dargestellt. Der grundsätzliche Aufbau aus Kupfer-Grundkörper (2; S), Eisen^-Zwischenschicht (3; 7) und Weissmetall-Deckschicht (4; 8) als Lauffläche erklärt sich von selbst.In Fig. 3 a section through the layer sequence of an IQ bearing body is shown. The basic structure of the copper base body (2; S), iron ^ intermediate layer (3; 7) and white metal top layer (4; 8) as a running surface is self-explanatory.
Durch die Neuerung wird es möglich, bei Gleitlagern auf der Basis von Zinn-WeissHietall durch wesentliche Verbesserung der Wärmeabfuhr über einen Grundkörper (Stützkörper) aus Kupfer oder einer Kupferlegierung gegenüber Eisenlegierungen (Stahl, Gusseisen) die Belastbarkeit zu erhöhen, ohne eine betriebsbedingte Versprödung und vorzeitige Rissbildung in der intermetallischen Bindungszone zwischen Weissmetall und Trägermetall in Kauf nehmen zu müssen. Dank der fest haftenden Eisen-Zwischenschicht zwischen Lagermetall und Stützkörper wird eine hohe Betriebssicherheit und lange Lebensdauer auch bei hohen Belastungen der Läger gewährleistet.The innovation makes it possible to significantly improve slide bearings based on tin-white hietall the heat dissipation via a base body (support body) made of copper or a copper alloy compared to iron alloys (Steel, cast iron) to increase the load capacity without operational embrittlement and premature Having to accept crack formation in the intermetallic bond zone between white metal and carrier metal. thanks to the firmly adhering iron intermediate layer between the bearing metal and the support body ensures a high level of operational reliability and a long service life is guaranteed even with high loads on the bearings.
(. t* ** *t t tt ti (. t * ** * tt tt ti
feezeichnungsiistefee drawing list
1 = Radiallager-Häibschäle1 = radial bearing cups
2 - Kupfermantel als örundkörper2 - copper jacket as an orbital body
3 - Eisen-Zwischenschicht (zylindrisch)3 - intermediate iron layer (cylindrical)
4 = Weissmetall-Aüsgüss als Deckschicht4 = White metal cast as a top layer
(zylindrisch)(cylindrical)
5 = Axiallager-Kreis segment5 = axial bearing circle segment
6 = Kupferblock als Grundkörper6 = copper block as the base body
7 = Eisen-Zwischenschicht (eh?n)7 = iron intermediate layer (eh? N)
8 = Weissmetall-Deckschicht (eben)8 = white metal top layer (flat)
Claims (6)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH1051179 | 1979-11-27 |
Publications (1)
Publication Number | Publication Date |
---|---|
DE8001995U1 true DE8001995U1 (en) | 1981-05-21 |
Family
ID=1326149
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE8001995U Expired DE8001995U1 (en) | 1979-11-27 | Bearing body for a plain bearing with high thermal conductivity |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE8001995U1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4328920A1 (en) * | 1992-09-17 | 1994-04-07 | Daido Metal Co Ltd | Multi-layer plain bearings and bearing assembly |
-
0
- DE DE8001995U patent/DE8001995U1/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4328920A1 (en) * | 1992-09-17 | 1994-04-07 | Daido Metal Co Ltd | Multi-layer plain bearings and bearing assembly |
US5434012A (en) * | 1992-09-17 | 1995-07-18 | Daido Metal Company, Ltd. | Multilayer slide bearing and bearing assembly |
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